N712EV

Service difficulty reports · 251

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N712EV' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR ASOA2014112411747Panel · buckledPAX DOOR FWD AND AFT SIDEWALL PANELS BUCKLED. REMOVED SUPPORT STRUCTURE ON AFT SIDE PANEL. STIFFENER PN 601R317745-7, CRACKED REPLACE WITH NEW. FASTENERS REMOVED IAW SRM 51-42-06-001-001-A01/51-42-10-001-001-A01/51-42-22-001-001-A01. INSTALLED SUPPORT STRUNov 2, 2014 · N712EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA2014112411746Angle · corrodedFOUND CORROSION ON ASD KICKPLATE ANGLE. REMOVED KICKPLATE ANGLE IAW SRM 51-42-06-001-001-A01. DRILLED NR 21 HOLE AT FS 333 AND TRANSFERRED NR 46 PILOT NOT FROM MIDCAP TO KICKPLATE ANGLE 11EA AND 1EA, 21 TO CLIP FITTING. INSTALLED.Nov 1, 2014 · N712EV · Cndair CL6002C10 · Service DoorsSDR ASOA2014112411745Angle · damagedAFTER REMOVING FWD DRAG ANGLE ON PAX DOOR FOUND PREVIOUSLY OVERSIZED HOLE AROUND PANEL 832DL, CUTOUT. REPAIRED IAW REO 670-52-11-800, REV--, REO 670-52-11-806 REV--, AND EC/TC REO 670-52-11-800 .Oct 31, 2014 · N712EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014112411743Angle · corrodedSERVICE DOOR LOWER MOUNTING ANGLE CORRODED AND IS OUT OF LIMITS IAW SRM 53-21-23-101-002-A01. REMOVED MOUNTING ANGLE IAW SRM 51-42-21-001-001-A01 AND 51-40-06-001-001-A01. INSTALLED MOUNTING ANGLE IAW SRM 51-42-21-801-001-A01 AND 51-40-06-001-01-A01 AND DWG Oct 29, 2014 · N712EV · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR ASOA2014112411742Bulkhead Web · corrodedLT LOWER BS 280 BULKHEAD WEB CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-10-201-003-A01. REPAIRED IAW REO 670-53-11-594.Oct 27, 2014 · N712EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA2014112411741Bulkhead Web · corrodedRT LOWER BS 280 BULKHEAD WEB CORRODED. FOUND IT TO BE OUT OF LIMITS IAW SRM 53-11-10-201-003-A01. REPAIRED IAW EC/TC REO 670-53-11-594 01 AND GREO 670-53-11-594 REV-.Oct 27, 2014 · N712EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA2014112411740Intercostal · corrodedINTERCOSTAL HAS CORROSION AT BS 364. REMOVED CORROSION IAW SRM 5121-06-001-001-A01.Oct 27, 2014 · N712EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014112411739Frame · corrodedFRAME BS 319 HAS CORROSION BETWEEN STRINGER 25-27R. REMOVED CORROSION IAW SRM 53-21-06-101-002-A01.Oct 27, 2014 · N712EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA2014112411738Stringer · corrodedSTRINGER 26R HAS CORROSION BETWEEN FS 333 TO 349. REMOVE CORROISON IAW SRM 53-21-03-101-002-A01. REMOVED CORROSION IAW SRM 53-21-23-101-003-A01 AND SRM 51-1-23-101-003-A01 AND SRM 51-21-06-001-001-A01. BLENDED AREA IS OUT OF LIMITS IAW SRM 53-21-23-101-003Oct 27, 2014 · N712EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2014112411737Stringer · corrodedSTRINGER 25R HAS CORROSION BETWEEN 310 TO 333. REMOVED CORROSION AND FOUND DAMAGE 3TO BE BEYOND LIMITS, CORROSION IS THROUGH STR 25R IAW SRM 53-21-03-101-002-A01, 51-24-06-001-001-A01. R & R STRINGER 25R FS280-349 IAW SRM 51-42-21-001-001-A01 AND 51-42-06-00Oct 27, 2014 · N712EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2014112411736Doubler · corrodedANTENNA DOUBLER HAS CORROSION IN AVIONICS BAY BETWEEN BS 295 - 310. REPLACED TCAS DOUBLER WITH SERIVCEABLE TCAS DOUBLER IAW SRM 51-4-06-001-001-A01 AND 51-42-21-001-001-A01. LOCATED AND DRILLED NEW TCAS DOUBLER IAW SRM 51-40-11-001-001-A01.Oct 27, 2014 · N712EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA2014112411735Stringer · corrodedSTRINGER 25R HAS CORROSION BETWEEN BS 333 TO 349. REMOVED CORROSION AND FOUND DAMAGE IS BEYOND LIMITS, CORROISON IS COMPLETELY THROUGH DTGR 25T IAW SRM 53-21-03-101-006-A01, 51-21-06-001-001-A01. REPLACED STR 25R SPLICE BETWEEN FS 333-FS349. REMOVED STR25R Oct 27, 2014 · N712EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2014112411734Stringer · corrodedSTRINGER 26R HAS CORROSION BETWEEN FRAMES 295 TO 333. REMOVED CORROSION BETWEEN FRAMES 295-333 ON STR 26R IAW SRM 53-21-03-101-002-A01, 51-21-06-001-001-A01. BLENDED AREAS ARE OUT OF ALLOWABLE LIMITS IAW SRM 53-21-06-101-002-A01. INSTALLED STRINGER TO ORGOct 27, 2014 · N712EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2014112411733Strap · corrodedBELLY FS 280, STRAP HAS CORROSION BETWEEN STRINGERS 26L-26R. REMOVED CORROSION IAW SRM 57-21-06-001-001-A01.Oct 27, 2014 · N712EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014112411732Floorbeam · corrodedAVIONICS BAY FLOORBEAM HAS CORROSION AT BS 280. R & R FLOORBEAM ANGLE IAW SRM 51-42-06-001-001-A01, 51-40-11-001-0001-A01, 51-42-21-001-001-A01.Oct 27, 2014 · N712EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2014112411731Frame · corrodedFRAME BS 295 HAS CORROSION BETWEEN STRINGERS 25L-25R. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01 AND 53-21-06-101-002-A01. COMPLIED WITH GREO 690-53-21-799.Oct 27, 2014 · N712EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA2014112411730Hinge · gougedFUSELAGE SIDE PAX DOOR HINGE, AFT LUG, QOUGED BY ROLL PIN. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. COMPLIED WITH ECTC GREO 670-53-21-582 AND TYPE I DISPOSIITION REO 670-53-21-582. ECTC COMPLIED WITH REPAIRED PASSENGER DOOR HINGE, FUSELAGE Oct 27, 2014 · N712EV · Cndair CL6002C10 · Fuselage, Door HingeSDR ASOA2014112411729Track · bentFWD/AFT, AFT CARGO DOOR, DOOR TRACKS HAVE IMPACT DAMAGE, BENT, PREVENTING DOOR FROM OPERATING SMOOTHLY OPEN, AS MARKED. RECEIVED FINAL EA 32-2014-177 AND EA 32-2014-167. RESHAPED AND CONTOURED IAW ENGINEERING REQUEST AND BLENDED GOUGES AND DENTS IAW SRM 51-Oct 27, 2014 · N712EV · Cndair CL6002C10 · Cargo/Baggage DoorsSDR ASOA2014112411728Structure · corrodedPACKER CORRODED LBL9 APPROXIMATELY FS 333. R & R PACKER IAW DWG SH670-32120, SRM 51-42-06-001-001-A01. SDR CLOSED.Oct 26, 2014 · N712EV · Cndair CL6002C10 · Fuselage Main, StructureSDR ASOA2014112411727Floor Support · corrodedRBL 45 SILL CORRODED FS 285 AND APP FS 300-319. REMOVED CORROSION ON RT FLOOR SILL STA 285-319 IAW SRM 51-21-06-001-001-A01. CORROSION OUT OF LIMITS BY VISUAL INSP EXFOLIATION THROUGH PART. REMOVED FS 280-FS 477.40 FLOOR SILL STRUCTURE RT AND BEGAN DRILLING Oct 26, 2014 · N712EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014112411726Structure · corrodedPACKER CORRODED RBL9 APPROXIMATELY FS 349. R & R PACKER IAW DWG SH670-32120, SRM 51-42-06-001-001-A01.Oct 26, 2014 · N712EV · Cndair CL6002C10 · Fuselage Main, StructureSDR ASOA2014112411725Floor Support · corrodedFLOOR SUPPORT CORRODED RBL45 AT FS 349 AND SMALL AREA AT APPROXIMATELY FS 385. COMPLIED WITH GREO 670-53-00-390. COMPLIED WITH ECTC REO 670-53-00-370 AND REO 670-53-00-390, REV -- DATED 01/22/2014.Oct 26, 2014 · N712EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014112411724Door Sill · corrodedASD SILL ANGLE CORRODED. AFTER EVALUATION OF MIDCAP ANGLE DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-001-A01. REMOVED MIDCAP ANGLE IAW SRM 51-42-06-001-001-A01. DRILLED 11 PILOT HOLES IN MIDCAP ANGLE WITH NR 40 DRILL BIT IAW SRM 51-40-11-001-001-Oct 26, 2014 · N712EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014112411723Seat Track · corrodedFS 349-485, RBL9 SEAT TRACK CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03. RECEIVED AND COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV G AS WRITTEN. LOCOct 26, 2014 · N712EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014032810209Retainer · bentSEAL RETAINER FWD CARGO DOOR BENT. COMPLIED WITH EC/TC REO 670-52-35-127. MAJOR REPAIR IAW GMM 5-3.Mar 25, 2014 · N712EV · Cndair CL6002C10 · Cargo/Baggage DoorsSDR ASOA2013110809377Flashlight · inoperativeCAPTAIN'S FLASHLIGHT INOPERATIVE. REPAIRED FLASHLIGHT IAW GMM 3-8. OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED.Nov 7, 2013 · N712EV · Cndair CL6002C10 · Emergency EquipmentSDR ASOA2013040503318Seal · dirtySERVICE DOOR DIFFICULT TO OPEN AND CLOSE. CLEANED AND LUBED DR SEAL OPS CKED GOOD IAW AMM 52-41-02.Apr 4, 2013 · N712EV · Cndair CL6002C10 · Service DoorsSDR ASOA2013012102858Battery · dischargedAFT F/A'S FLASHLIGHT INOPERATIVE. R & R BATTERIES IAW AMM 25-61-02. OPS CHECK GOOD NO FURTHER DEFECTS NOTED AT THIS TIME.Jan 16, 2013 · N712EV · Cndair CL6002C10 · Emergency EquipmentSDR ASOA2012121802672Angle · corrodedANGLES AT HINGE SIDE OF PAX DOOR. R & R IAW SRM 51-42-06-001-001-A01.Nov 26, 2012 · N712EV · Cndair CL6002C10 · Fuselage, Door HingeSDR ASOA2012121802671Bulkhead Web · corrodedLEFT SIDE FS 280 LOWER BULKHEAD WEB HAS CORROSION DAMAGE. REPAIRED IAW REO 670-53-11-594.Nov 21, 2012 · N712EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA2012121802670Floorbeam · corrodedCOCKPIT FLOORBEAM AT FS 280 IS CORRODED. REMOVED ANGLE IAW SRM 51-42-21. FABRICATED NEW FLOORBEAM BY MATCH DRILLING TO EXISTING FASTENER HOLES IN ACFT AND OLD ANGLE. INSTALLED IAW SRM 51-42-21, 51-42-06 AND 51-42-13.Nov 21, 2012 · N712EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2012121802669Frame · corrodedFRAME BS 310 CORRODED AT STRINGER 27 FWD & AFT SIDES. BLENDED CORRODED AREA IAW SRM 51-42-06. BLENDED CORRODED AREA IAW SRM 51-21-06-001-001-A01. COMPLIED WITH REO 670-53-21-907.Nov 19, 2012 · N712EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA2012121802668Stringer · corrodedSTRINGER 27 CORRODED BETWEEN FRAMES 333 AND 349. COMPLETED REPAIR IAW REO 670-53-21-261.Nov 19, 2012 · N712EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2012121802667Doubler · corrodedTCAS DOUBLER CORRODED UNDER FLOOR AT STRINGER 27 BETWEEN FRAMES BS 295 AND 310. REMOVED TCAS DOUBLER IAW SRM 51-42-06 BECAUSE DOUBLER WAS CORRODED OUT OF LIMITS IAW SRM 53-21-01. INSTALLED NEW TCAS DOUBLER BETWEEN FRAME 295 AND 310 IAW SRM 51-42-06.Nov 19, 2012 · N712EV · Cndair CL6002C10 · Fuselage Main, StructureSDR ASOA2012121802666Frame · corrodedFRAME BS 295 CORRODED BETWEEN STGR 26R AND STGR26L. BLENDED FRAME IAW SRM 51-21-06-001-001-A01. COMPLIED WITH REO 670-53-21-908.Nov 19, 2012 · N712EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA2012121802665Attach Bracket · crackedVERTICAL STAB TO FUSELAGE LT CHANNEL BRACKET CRACKED ABOVE APU DOOR. REPAIRED IAW REO 670-55-31-062.Nov 19, 2012 · N712EV · Cndair CL6002C10 · Vertical Stabilizer, Attach FittingsSDR ASOA2012112802554Floorbeam · corrodedFWD FLOORBEAM ANGLE CORRODED. R & R FLOORBEAM ANGLE BS 280 IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.Nov 19, 2012 · N712EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2012112802553Floor Panel · crackedFWD EQUIPMENT COMPARTMENT FLOOR CRACKED. COMPLIED REO 670-523-11-509.Nov 19, 2012 · N712EV · Cndair CL6002C10 · Fuselage Floor PanelSDR ASOA2012121802664Crossbeam · corrodedLEFT SIDE FS 280 CROSSBEAM HAS CORROSION DAMAGE. FS 280 CROSSBEAM R & R IAW REO 670-53-11-047.Nov 16, 2012 · N712EV · Cndair CL6002C10 · Fuselage Main, StructureSDR ASOA2012121402658Floor Support · corrodedRT SIDE FLOOR SUPPORT HAS CORROSION DAMAGE AT APPROX FS 1050.00 AROUND NUTPLATE. FOUND THAT THE CORROSION EXTEND FWD TO FS 1031.00. RECEIVED AND COMPLIED WITH REO 670-53-61-921.Nov 16, 2012 · N712EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012121402660Crossbeam · corrodedRT SIDE FS 280 CROSSBEAM HAS CORROSION DAMAGE. RECEIVED AND COMPLIED WITH EC/TC REO 670-53-11-047 AND REO 670-53-11-047, REV E DATED 8/13/09. REPAIR CLASSIFIED AS MAJOR.Nov 16, 2012 · N712EV · Cndair CL6002C10 · Fuselage Main, StructureSDR ASOA2012121402659Bulkhead · corrodedRT SIDE FS 280 LOWER BULKHEAD WEB HAS CORROSION DAMAGE. RECEIVED AND COMPLIED WITH EC/TC REO 670-53-11-594 AND GENERIC REO 670-53-11-594 REV-DATED 04/27/2011.Nov 16, 2012 · N712EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA2012121402657Floor Support · corrodedRT SIDE FLOOR SUPPORT HAS CORROSION DAMAGE AT FS 1051.30. CORROSION WAS FOUND TO EXTEND AFT FROM FS 1051.3 TO APPROX 1061.00. COMPLIED WITH REO 670-53-61-921.Nov 16, 2012 · N712EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012081002052Skin · crackedAFT REPAIR ON PAX DOOR, UPPER CORNER, CRACKED. WORK COMPLETED IAW N/R -00004. UPON FURTHER INVESTAGATION FOUND PREVIOUS REPAIR REO 601R-52-11-279 REPAIR DOUBLER CRACKED ONLY. R & R WITH NEW DOUBLER IAW REO 601R-52-11-279.Aug 7, 2012 · N712EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA2012081002051Skin · crackedFWD REPAIR ON PAX DOOR, UPPER CORNER, CRACKED. WORK COMPLETED IAW N/R, ITEM: 1. UPON FURTHER INVESTAGATION, FOUND PREVIOUS REPAIR REO 601R-52-11-279. REPAIR DOUBLER CRACKED ONLY. R & R WITH NEW DOUBLER. REF REO 601R-52-11-279.Aug 7, 2012 · N712EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA201201322Landing Gear · noneGEAR DISAGREE AFTER SELECTING UP. RT MAIN GEAR SHOWED NOT RETRACTED. ACFT RETURNED TO DEPARTURE AND AN EMERGENCY DECLARED. PERFORMED FUNCTIONAL TEST OF LANDING-GEAR EXTENSION/RETRACTION SYS IAW AMM 32-30-00. OPS CHECK GOOD. NO DEFECTS NOTED.Apr 22, 2012 · N712EV · Cndair CL6002C10 · Landing Gear Retraction/Extension SystemSDR ASOA201200710Flashlight · unserviceableFLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW AMM 25-60-00. OPS CHECKED GOOD, NO FURTHER DEFECTS NOTED, ACFT OK FOR SERVICE.Mar 4, 2012 · N712EV · Cndair CL6002C10 · Emergency EquipmentSDR ASOA201101231Megaphone · inoperativeAFT CABIN MEGAPHONE INOPERATIVE AND DENTED. R & R AFT CABIN MEGAPHONE IAW AMM 25-61-14. OPS CHECKED GOOD.Jun 25, 2011 · N712EV · Cndair CL6002C10 · Emergency EquipmentSDR ASOA201001858Battery Pack · weakNR 4 EMERGENCY BATTERY WEAK. REPLACED THE EMERGENCY BATTERY PACK NR 4 AND PERFORMED OPS CHECK GOOD REF AMM TASK 33-51-04-400-801, 33-51-04-000-801 AND 33-51-06-740-801.Dec 2, 2010 · N712EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201001821Stringer · cracked3L STRINGER CRACKED AT FS280 AFT OF BULKHEAD. COMPLY WITH STEPS 5-11 OF REO670-53-21-493. COMPLIED WITH STEPS 5-10 OF REO 670-53-21-493. COMPLIED WITH STEP 11 OF REO 670-53-21-493 IAW DEVIATION REO 670-53-21-618.Nov 18, 2010 · N712EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
Back to N712EV